Titanium Alloy, Forgings 6.0Al - 2.0Sn - 4.0Zr - 2.0Mo Solution and Precipitation Heat Treated
- Aerospace Material Specification
- AMS4976G
- Revised
Scope
Rationale
Recommended Content
| Aerospace Material Specification | Titanium Alloy, Forgings 5Al - 2.5Sn Annealed, 110 ksi (758 MPa) Yield Strength |
| Aerospace Material Specification | Titanium Alloy Forgings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized |
Topic
Data Sets - Support Documents
| Title | Description | Download |
|---|---|---|
| Unnamed Dataset 1 | ||
| Unnamed Dataset 2 | ||
| TABLE 1 | COMPOSITION | |
| TABLE 2 | MINIMUM ROOM TEMPERATURE TENSILE PROPERTIES | |
| TABLE 3 | MINIMUM ELEVATED TEMPERATURE TENSILE PROPERTIES |
Issuing Committee
AMS G Titanium and Refractory Metals Committee
The committee of Titanium, Beryllium, and Refractory Materials, AMS Committee G, is responsible for preparation, revision, review and approval of documents related to aerospace application of these materials. Included are titanium, beryllium, and refractory metallic such as molybdenum, tantalum, and columbium. The committee provides a forum for interchange of experience and ideas among industry representatives, both suppliers and users, along with interested government agencies, to ensure the utility, proper technical content, and industry acceptance of published documents.